| Number |
2022-0037 |
| Issued by |
 Europe |
| Issue date |
2022-03-15 |
| Effective date |
2022-03-21 |
| EASA approval number |
|
| ATA Chapter |
62 |
Approval Holder
/ Type Designation |
-
LEONARDO S.p.A. HELICOPTERS
-
A109/A119
-
A109E
-
A109LUH
-
A109S
-
A119
-
AW109SP
-
AW119MKII
|
| Revision |
Not applicable
|
| Correction |
This AD is re-published to correct the Note reference in Table 2.
|
| Supersedure |
None
|
| Publication(s) and related information |
Leonardo ASB 109EP-177 original issue dated 11 January 2022, or Revision A dated 03 March 2022.
Leonardo ASB 109L-117 original issue dated 11 January 2022, or Revision A dated 03 March 2022.
Leonardo ASB 109S-105 original issue dated 11 January 2022, or Revision A dated 03 March 2022.
Leonardo ASB 109SP-149 original issue dated 11 January 2022, or Revision A dated 03 March 2022.
Leonardo ASB 119-111 original issue dated 11 January 2022, or Revision A dated 03 March 2022.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
22-005 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 24 January 2022 as PAD 22-005 for consultation until 21 February 2022. The Comment Response Document can be found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this AD.
3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
4. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on a product, part or appliance not affected by this AD, can be reported to the EU aviation safety reporting system. This may include reporting on the same or similar components, other than those covered by the design to which this AD applies, if the same unsafe condition can exist or may develop on an aircraft with those components installed. Such components may be installed under an FAA Parts Manufacturer Approval (PMA), Supplemental Type Certificate (STC) or other modification.
|
